NSN 3040-00-893-4546

Part Details | RIGID CONNECTING LINK

3040-00-893-4546 An item of various cross-sectional shapes which may be of solid or hollow construction. It is specifically designed for attachment to a lever(s) and/or control(s) to actuate various remote mechanisms. It is one of the following: (1) A one-piece item with or without eyes and/or holes in each end which may have bushings or bearings pressed in the eyes; (2) A one-piece item with both ends processed for terminations, excluding threaded end(s); (3) A two-piece construction type item consisting of a body with both ends processed for terminations and a single end attachment; or (4) A three-piece construction type item consisting of a body and two end attachments. Excludes internal combustion engine type piston connecting rods; DRAG LINK, STEERING; LINK, ANCHOR, BRAKE SHOE; TIE ROD, STEERING; and TURNBUCKLE. For cylindrical shaped externally threaded items without end attachments, see ROD, THREADED END and STUD (as modified).

Alternate Parts: 20400101277, 204-001-012-77, 204001012077, 204-001-012-077, 3040-00-893-4546, 00-893-4546, 3040008934546, 008934546

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
30JAN 01, 196000-893-454621988 ( CONNECTING LINK, RIGID )
REFERENCE DRAWINGS & PICTURES

ANGLED

Cross Reference | NSN 3040-00-893-4546
Part Number Cage Code Manufacturer
204-001-012-7797499BELL HELICOPTER TEXTRON INC.DBA BELL HELICOPTER
204-001-012-07797499BELL HELICOPTER TEXTRON INC.DBA BELL HELICOPTER
Technical Data | NSN 3040-00-893-4546
Characteristic Specifications
MATERIAL ALUMINUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATIONWW-T-785, T3, TY-1 CANCELED FED SPEC SINGLE MATERIAL RESPONSE
BODY CONSTRUCTION TUBULAR
LINK STYLE1 ANGLED
OVERALL LENGTH43.178 INCHES NOMINAL
BODY DIAMETER1.250 INCHES NOMINAL
SPECIAL FEATURESEFFECTIVE LENGTH: 42.500 INCHES; END ATTACHMENT INFO: MATERIAL ALUMINUM BOTH ENDS, SURFACE TREATMENT CHEMICAL FILM, FORK DEPTH 2.490 TO 2.500 INCHES, HEIGHT 0.706 INCH 1ST END, 0.650 INCH 2ND END, FORK SPAN WIDTH 0.817 INCH 1ST END, 0.692 INCH 2ND END; USED ON FORWARD FUSELAGE SECTION, AIRCRAFT